Autonomous Labs in Space for

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[ PRODUCTS ]
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End-to-End Space Infrastructure Under One Roof.\

The only company in the world, from the tip of the rockets (deployers) to spacecraft to data (ground stations), fully vertically integrated.
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Cosmotron\

The Cosmotron is a 50 kg class, fully vertically integrated spacecraft platform designed for rapid deployment in various space applications.

Fully Integrated Platform

Consolidates OBC (On-Board Computer), EPS (Electrical Power System), Communications, and Edge Computing onto a single PCB.

Reduces weight, complexity, and launch costs.

Flexible Payload Interfaces

Supports both hosted and dedicated payloads.

Designed for scalability and modularity.

AI-Driven Edge Computing

Enables real-time data processing in space.

Supports advanced AI algorithms for mission autonomy.

High-Speed Communication

Ensures efficient data transfer for space applications.

Supports low-latency connectivity.

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Applications:
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Technology Demonstration\

Validating new space technologies.
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Earth Observation\

High-resolution imaging and remote sensing.
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Scientific Research\

Supporting microgravity experiments and deep space studies.
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Designed for the New Space Economy!\

The Cosmotron Bus offers a scalable, modular, and cost-effective solution for emerging space missions, making it a versatile choice for commercial, scientific, and exploratory endeavors.

Class:

Quarter Plate

Spacecraft Mass:

50kg

Payload Capacity:

20-30 kg

Payload Volume:

Modular

In-Orbit Average Power:

100W

Bus Voltage:

5V, 12V, 32V (Customization Available)

Pointing Accuracy:

<100" (3-sigma)

Standard In-Orbit Demo Duration:

6 months - 1 year

Data Storage:

64GB EDAC-protected

Edge Computing:

Onboard GPU for Al & data processing

Communication:

UHF, S-Band, X-Band

Data Rates:

Up to 10 Mbps Downlink & Up to 1 Mbps Uplink

Payload Interfaces:

CAN, RS422/RS485, UART, Ethernet, I2C, SPI(Customization Available), SpaceWire

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Class:

0.5m class

Mass:

27kg

Payload Mass:

5kg

Payload Volume:

4U (Pressurized)

Maximum Entry Gs:

<15

Communications:

Iridium

Mission Duration:

<3 Months

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REX(50)\

REX(100)\

REX (100) features a viewport for plasma dynamics observation during hypersonic atmospheric reentry and precision capsule delivery using guided parafoils.

Class:

1m class

Mass:

85kg

Payload Mass:

10kg

Payload Volume:

12U (Pressurized)

Maximum Entry Gs:

<15

Communications:

Iridium

Mission Duration:

3-6 Months

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Mass of System:

380gm

Mass of Sequencer:

160gm

Payload Mass:

~3.5kg (Maximum)

Payload cf envelope:

X-Axis 80mm, Y-Axis 80mm, Z-Axis 120mm (from the base)

Hold down and release mechanism:

Burn Wire

Separation Velocity:

1 m/s to 3 m/s (configurable)

Operating Temperature:

-15 C TO +60 C

Compatibility:

Every Launch Vehicle

Standard:

Cubesat NextGen

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DEPLOYER-X\

DeployerX is a non-canisterised, pin-based separation system developed for nanosatellites. It follows our in-house developed next-generation CubeSat standard (CubeSat NG), allowing customers to benefit from a lighter separation system mass. This results in lower launch costs and the ability to accommodate unrestricted volume in satellite structures.

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Let's Do This.\

Just talking won't get you to space, action will. We've done it 26 times already,one more won't hurt.If you're serious, we should talk.

2 Marina Blvd B300, San Francisco, California 94123, US.

2 Marina Blvd B300

2 Marina Blvd B300, San Francisco, CA 94123, USA

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